TM 1-1510-225-10 7-96 MAXIMUM RANGE POWER 1700 RPM ISA + 20 °C NOTES: DURING   OPERATION   WITH   ICE   VANES  E XTENDED,   TORQUE   WILL   DECREASE.      IN ORDER  TO  MAINTAIN  MAXIMUM  RANGE  CONFIGURATION,  DO  NOT  RESET  POWER TO ORIGINAL SETTING.  FUEL FLOW WILL REMAIN ABOUT THE SAME, BUT TRUE AIRSPEED WILL BE REDUCED APPROXIMATELY 10 KNOTS. TO OBTAIN FUEL FLOW PER ENGINE, DIVIDE  THE TOTAL FUEL FLOW  VALUE FOR THE CORRESPONDING ALTITUDE BY TWO. WEIGHT  Ü  13,000 POUNDS 12,000 POUNDS PRESSURE ALT IOAT OAT TORQUE PER ENGINE FUEL FLOW TOTAL IAS TAS TORQUE PER ENGINE FUEL FLOW TOTAL IAS TAS FEET °C °C FT-LB % LB/HR KTS KTS FT-LB % LB/HR KTS KTS SL 39 35 1628 73 810 205 213 1583 71 798 204 212 2,000 35 31 1606 72 722 201 215 1539 69 758 200 214 4,000 31 27 1561 70 734 197 217 1539 69 726 197 217 6,000 28 23 1539 69 698 193 219 1494 67 688 193 219 8,000 24 19 1494 67 660 188 220 1450 65 650 188 221 10,000 20 15 1450 65 622 183 222 1405 63 610 183 222 12,000 16 11 1405 63 588 179 223 1360 61 578 179 223 14,000 12 7 1383 62 562 174 224 1338 60 550 175 225 16,000 8 3 1360 61 538 170 226 1316 59 526 171 227 18,000 4 -1 1338 60 516 166 228 1293 58 504 167 229 20,000 0 -5 1338 60 502 163 231 1293 58 488 163 232 22,000 -3 -9 1316 59 490 159 234 1271 57 472 159 234 24,000 -7 -13 1338 60 484 157 239 1227 55 452 154 234 26,000 -11 -17 1360 61 484 156 245 1227 55 444 151 238 28,000 -15 -21 1360 61 480 152 247 1249 56 446 149 244 29,000 -17 -22 – – – – – – – – – – – – – – – 1249 56 444 147 245 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7-87.  Maximum Range Power, 1700 RPM, ISA + 20 °C (Sheet 1 of 2)